INTELSAT 3R (PAS 3R), 23764
Orbit data source: Space-Track
INTELSAT 3R (PAS 3R), 23764 is a payload satellite owned by Panamsat (US) in GEO that was launched on Fri, 12 Jan 1996 UTC via an ARIANE 44L launch vehicle from the French Guiana (FRGUI). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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23764 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Hughes
Mission
Non-operational Commercial Communications
Bus & Motor
HS-601, R-4D-11-300
Mass
2,918 kg wet, 1,318 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Hex Poly + 2 Pan, 13.0 m
Radar Cross Section
73.695 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 INTELSAT 3R (PAS 3R)
1 23764U 96002A 26140.56037028 -.00000199 00000-0 00000-0 0 9993
2 23764 11.7048 37.0346 0012095 291.2110 287.6380 0.99091595110510Epoch: 2026-05-20T13:26Z
TLE epoch observation values (Epoch: 2026-05-20T13:26:55.992Z)
Latitude
-7.31528°
Longitude
175.23144°
Altitude
36,106.04 km
Speed
3.064 km/s
True Right ascension
17h 00m 43s
True Declination
-7° 18' 29"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
01:05:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,173.126 km
Perigee altitude
36,070.319 km
Semi-major axis
42,499.86 km
Eccentricity
0.00121
Inclination
11.7048°
RAAN
37.0346°
Arg. of periapsis
291.211°
True anomaly
287.50586°
Mean anomaly
287.638°
Eccentric anomaly
287.57193°
Mean motion
0.24772 °/min
Orbital period
1,453.25 mins
BSTAR
0
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Other satellites on launch #2 in the year 1996 (1996-01-12 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.INTELSAT 3R (PAS 3R) Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| INTELSAT 3R (PAS 3R) is likely not visible in the next few days. |
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23764 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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